Vacuum adiabatic body and refrigerator

ABSTRACT

A vacuum adiabatic body and a refrigerator are provided. The vacuum adiabatic body includes a support that maintains a vacuum space between a first plate and a second plate. The support includes a first support plate provided by coupling at least two partial plates to support one of the first plate or the second plate, and a second support plate that supports the other one of the first plate or the second plate.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Continuation application of U.S. patentapplication Ser. No. 16/637,861 filed Feb. 10, 2020, which is a U.S.National Stage Application under 35 U.S.C. § 371 of PCT Application No.PCT/KR2018/008700, filed Jul. 31, 2018, which claims priority under 35U.S.C. § 119 to Korean Application No. 10-2017-0103444, filed Aug. 16,2017, whose entire disclosures are hereby incorporated by reference.

BACKGROUND 1. Field

A vacuum adiabatic body and a refrigerator are disclosed herein.

2. BACKGROUND

A vacuum adiabatic body is a product for suppressing heat transfer byvacuumizing an interior of a body thereof. The vacuum adiabatic body mayreduce heat transfer by convection and conduction, and hence is appliedto heating apparatuses and refrigerating apparatuses. In a typicaladiabatic method applied to a refrigerator, although it is differentlyapplied in refrigeration and freezing, a foam urethane adiabatic wallhaving a thickness of about 30 cm or more is generally provided.However, an internal volume of the refrigerator is therefore reduced.

In order to increase the internal volume of a refrigerator, there is anattempt to apply a vacuum adiabatic body to the refrigerator.

First, Korean Patent No. 10-0343719 (Reference Document 1) of thepresent applicant has been disclosed. According to Reference Document 1,there is disclosed a method in which a vacuum adiabatic panel isprepared and then built in walls of a refrigerator, and an exterior ofthe vacuum adiabatic panel is finished with a separate molding asStyrofoam. According to the method, additional foaming is not required,and adiabatic performance of the refrigerator is improved. However,fabrication cost is increased, and a fabrication method is complicated.As another example, a technique of providing walls using a vacuumadiabatic material and additionally providing adiabatic walls using afoam filling material has been disclosed in Korean Patent PublicationNo. 10-2015-0012712 (Reference Document 2). According to ReferenceDocument 2, fabrication cost is increased, and a fabrication method iscomplicated.

As further another example, there is an attempt to fabricate all wallsof a refrigerator using a vacuum adiabatic body that is a singleproduct. For example, a technique of providing an adiabatic structure ofa refrigerator to be in a vacuum state has been disclosed in U.S. PatentLaid-Open Publication No. US2040226956A1 (Reference Document 3).However, it is difficult to obtain a practical level of an adiabaticeffect by providing a wall of the refrigerator with sufficient vacuum.In detail, there are limitations in that it is difficult to prevent aheat transfer phenomenon at a contact portion between an outer case andan inner case having different temperatures, it is difficult to maintaina stable vacuum state, and it is difficult to prevent deformation of acase due to a negative pressure of the vacuum state. Due to theselimitations, the technology disclosed in Reference Document 3 is limitedto a cryogenic refrigerator, and does not provide a level of technologyapplicable to general households.

The present applicant had filed Korean Patent Application No.10-2015-0109727 in consideration of the above-described limitations. Inthe above document, a refrigerator including a vacuum adiabatic body isproposed. Particularly, a resin material that is adequate for a materialfor forming a supporting unit of the vacuum adiabatic body is proposed.Even in this document, there is a limitation that a shape of thesupporting unit is different from that of the design, and it isdifficult to manufacture and handle the supporting unit, and yield ofthe product is low.

Embodiments provide a vacuum adiabatic body, in which a shape of asupporting unit is maintained in a designed shape, and a refrigerator.Embodiments also provide a vacuum adiabatic body, which is easy inmanufacturing and handling, and a refrigerator. Embodiments also providea vacuum adiabatic body, in which defective factors occurring when asupporting unit is manufactured are reduced to improve yield of aproduct, and a refrigerator.

In order to allow a shape of a supporting unit provided in a vacuumadiabatic body to be maintained in a designed shape, the supporting unitmay include one side support plate and the other side support plate,which respectively support plate members, and the one side support platemay be provided by coupling at least two plates to each other so thatthe member has a small size. In order to easily manufacture and handlethe supporting unit, a partial plate may have a rectangular shape, and afemale coupling structure and a male coupling structure may be providedon the edge of the partial plate.

In order to improve yield of the supporting unit, at least one of theone side support plate and the other side support plate may be providedby coupling at least two members having the same shape, which areseparated from each other in an extension direction of the correspondingplate member. Also, a large-sized plate member may be cut to be used.

The details of one or more embodiments are set forth in the accompanyingdrawings and the description below. Other features will be apparent fromthe description and drawings, and from the claims.

According to embodiments, there may be an advantage that the shape ofthe supporting unit is manufactured correctly, and a finish andreliability of the product are improved. Also, parts may be shared toreduce stock. According to embodiments, small parts manufactured andtransported to be assembled so as to manufacture a large-sized part, sothat manufacturing and handling of the supporting unit are simple andeasy. According to embodiments, it is possible to improve productionyield of the supporting unit by applying the parts even if moldability,i.e., the resin having poor melt mobility is used. Further, even in thecase of defective molding, only the parts need to be discarded, so thatproduction yield of the supporting unit may be improved.

BRIEF DESCRIPTION OF THE DRAWINGS

Embodiments will be described in detail with reference to the followingdrawings in which like reference numerals refer to like elements, andwherein:

FIG. 1 is a perspective view of a refrigerator according to anembodiment;

FIG. 2 is a view schematically showing a vacuum adiabatic body used in amain body and a door of the refrigerator;

FIGS. 3A-3B are views illustrating various embodiments of an internalconfiguration of a vacuum space part;

FIG. 4 is a diagram illustrating results obtained by examining resins;

FIG. 5 illustrates results obtained by performing an experiment onvacuum maintenance performances of resins;

FIGS. 6A-6C are results obtained by analyzing components of gasesdischarged from polyphenylene sulfide (PPS) and low outgassingpolycarbonate (PC);

FIG. 7 illustrates results obtained by measuring maximum deformationtemperatures at which resins are damaged by atmospheric pressure inhigh-temperature exhaustion;

FIGS. 8A-8C are views showing various embodiments of conductiveresistance sheets and peripheral parts thereof;

FIG. 9 is a view illustrating any one side portion of a supporting unitaccording an embodiment;

FIG. 10 is a plan view of a partial plate;

FIG. 11 is an enlarged view of a portion A of FIG. 10 ;

FIG. 12 is an enlarged view of a portion B of FIG. 10 ;

FIG. 13 is an enlarged view of a portion C of FIG. 9 ;

FIG. 14 is a view for explaining coupling between one side support plateand the other side support plate;

FIG. 15 is an enlarged view of a portion D of FIG. 14 ;

FIG. 16 is a cross-sectional view taken along line XVI-XVI′ of FIG. 15 ;

FIG. 17 is a view of a supporting unit according to another embodiment;

FIG. 18 illustrates graphs showing changes in adiabatic performance andchanges in gas conductivity with respect to vacuum pressures by applyinga simulation;

FIG. 19 is a graph illustrating results obtained by observing a time anda pressure in a process of exhausting the inside of the vacuum adiabaticbody when a supporting unit is used; and

FIG. 20 is a graph illustrating results obtained by comparing a vacuumpressure with gas conductivity.

DETAILED DESCRIPTION

Hereinafter, exemplary embodiments will be described with reference tothe accompanying drawings. The embodiments may, however, be embodied inmany different forms and should not be construed as being limited to theembodiments set forth herein, and a person of ordinary skill in the art,who understands the spirit, may readily implement other embodimentsincluded within the scope of the same concept by adding, changing,deleting, and adding components; rather, it will be understood that theyare also included within the scope.

The drawings shown below may be displayed differently from the actualproduct, or exaggerated or simple or detailed parts may be deleted, butthis is intended to facilitate understanding of the technical idea. Itshould not be construed as limited.

In the following description, the term vacuum pressure means anypressure state lower than atmospheric pressure. In addition, theexpression that a vacuum degree of A is higher than that of B means thata vacuum pressure of A is lower than that of B.

FIG. 1 is a perspective view of a refrigerator according to anembodiment. Referring to FIG. 1 , the refrigerator 1 includes a mainbody 2 provided with a cavity 9 capable of storing storage goods and adoor 3 provided to open/close the main body 2. The door 3 may berotatably or slidably movably disposed to open/close the cavity 9. Thecavity 9 may provide at least one of a refrigerating compartment or afreezing compartment.

Parts constituting a freezing cycle in which cold air is supplied intothe cavity 9. In detail, the parts include a compressor 4 thatcompresses a refrigerant, a condenser 5 that condenses the compressedrefrigerant, an expander 6 that expands the condensed refrigerant, andan evaporator 7 that evaporates the expanded refrigerant to take heat.As a typical structure, a fan may be installed at a position adjacent tothe evaporator 7, and a fluid blown from the fan may pass through theevaporator 7 and then be blown into the cavity 9. A freezing load iscontrolled by adjusting a blowing amount and blowing direction by thefan, adjusting an amount of a circulated refrigerant, or adjusting acompression rate of the compressor, so that it is possible to control arefrigerating space or a freezing space. Other parts constituting therefrigeration cycle may be constituted by applying a member including athermoelectric module.

FIG. 2 is a view schematically showing a vacuum adiabatic body used inthe main body and the door of the refrigerator. In FIG. 2 , a mainbody-side vacuum adiabatic body is illustrated in a state in which topand side walls are removed, and a door-side vacuum adiabatic body isillustrated in a state in which a portion of a front wall is removed. Inaddition, sections of portions at conductive resistance sheets areprovided are schematically illustrated for convenience of understanding.

Referring to FIG. 2 , the vacuum adiabatic body includes a first platemember (first plate) 10 for providing a wall of a low-temperature space,a second plate member (second plate) 20 for providing a wall of ahigh-temperature space, a vacuum space part (vacuum space) 50 defined asan interval part between the first and second plate members 10 and 20.Also, the vacuum adiabatic body includes conductive resistance sheets 60and 63 for preventing heat conduction between the first and second platemembers 10 and 20. A sealing part (sealing) 61 for sealing the first andsecond plate members 10 and 20 is provided such that the vacuum spacepart 50 is in a sealed state. When the vacuum adiabatic body is appliedto a refrigerator or a warming apparatus, the first plate member 10providing a wall of an inner space of the refrigerator may be referredto as an inner case, and the second plate member 20 providing a wall ofan outer space of the refrigerator may be referred to as an outer case.

A machine room 8 in which parts providing a freezing cycle areaccommodated is placed at a lower rear side of the main body-side vacuumadiabatic body, and an exhaust port 40 for forming a vacuum state byexhausting air in the vacuum space part 50 is provided at any one sideof the vacuum adiabatic body. In addition, a pipeline 64 passing throughthe vacuum space part 50 may be further installed so as to install adefrosting water line and electric lines.

The first plate member 10 may define at least one portion of a wall fora first space provided thereto. The second plate member 20 may define atleast one portion of a wall for a second space provided thereto. Thefirst space and the second space may be defined as spaces havingdifferent temperatures. The wall for each space may serve as not only awall directly contacting (facing) the space but also a wall notcontacting (facing) the space. For example, the vacuum adiabatic body ofthe embodiment may also be applied to a product further having aseparate wall contacting (facing) each space.

Factors of heat transfer, which cause loss of the adiabatic effect ofthe vacuum adiabatic body, are heat conduction between the first andsecond plate members 10 and 20, heat radiation between the first andsecond plate members 10 and 20, and gas conduction of the vacuum spacepart 50. Hereinafter, a heat resistance unit provided to reduceadiabatic loss related to the factors of the heat transfer will beprovided. The vacuum adiabatic body and the refrigerator of theembodiment do not exclude that another adiabatic means is furtherprovided to at least one side of the vacuum adiabatic body. Therefore,an adiabatic means using foaming, for example, may be further providedto another side of the vacuum adiabatic body.

FIGS. 3A-3B are views illustrating various embodiments of an internalconfiguration of the vacuum space part. Referring to FIG. 3A, the vacuumspace part 50 may be provided in a third space having a pressuredifferent from that of each of the first and second spaces, for example,a vacuum state, thereby reducing adiabatic loss. The third space may beprovided at a temperature between a temperature of the first space and atemperature of the second space. As the third space is provided as aspace in the vacuum state, the first and second plate members 10 and 20receive a force contracting in a direction in which they approach eachother due to a force corresponding to a pressure difference between thefirst and second spaces. Therefore, the vacuum space part 50 may bedeformed in a direction in which it is reduced. In this case, theadiabatic loss may be caused due to an increase in amount of heatradiation, caused by the contraction of the vacuum space part 50, and anincrease in amount of heat conduction, caused by contact between theplate members 10 and 20.

A supporting unit (support) 30 may be provided to reduce deformation ofthe vacuum space part 50. The supporting unit 30 includes a bar 31. Thebar 31 may extend in a substantially vertical direction with respect tothe plate members to support a distance between the first plate memberand the second plate member. A support plate 35 may be additionallyprovided on at least any one end of the bar 31. The support plate 35 mayconnect at least two or more bars 31 to each other to extend in ahorizontal direction with respect to the first and second plate members10 and 20. The support plate 35 may be provided in a plate shape or maybe provided in a lattice shape so that an area of the support platecontacting the first or second plate member 10 or 20 decreases, therebyreducing heat transfer. The bars 31 and the support plate 35 are fixedto each other at least one portion, to be inserted together between thefirst and second plate members 10 and 20. The support plate 35 contactsat least one of the first and second plate members 10 and 20, therebypreventing deformation of the first and second plate members 10 and 20.In addition, based on an extending direction of the bars 31, a totalsectional area of the support plate 35 is provided to be greater thanthat of the bars 31, so that heat transferred through the bars 31 may bediffused through the support plate 35.

A material of the supporting unit 30 will be described hereinafter.

The supporting unit 30 is to have a high compressive strength so as toendure the vacuum pressure. Also, the supporting unit 30 is to have alow outgassing rate and a low water absorption rate so as to maintainthe vacuum state. Further, the supporting unit 30 is to have a lowthermal conductivity so as to reduce heat conduction between the platemembers. Furthermore, the supporting unit 30 is to secure thecompressive strength at a high temperature so as to endure ahigh-temperature exhaust process. Additionally, the supporting unit 30is to have an excellent machinability so as to be subjected to molding.Also, the supporting unit 30 is to have a low cost for molding. A timerequired to perform the exhaust process takes about a few days. Hence,the time is reduced, thereby considerably improving fabrication cost andproductivity. Therefore, the compressive strength is to be secured atthe high temperature because an exhaust speed is increased as atemperature at which the exhaust process is performed becomes higher.The inventor has performed various examinations under theabove-described conditions.

First, ceramic or glass has a low outgassing rate and a low waterabsorption rate, but its machinability is remarkably lowered. Hence, theceramic and glass may not be used as the material of the supporting unit30. Therefore, resin may be considered as the material of the supportingunit 30.

FIG. 4 is a diagram illustrating results obtained by examining resins.Referring to FIG. 4 , the present inventor has examined various resins,and most of the resins cannot be used because their outgassing rates andwater absorption rates are remarkably high. Accordingly, the presentinventor has examined resins that approximately satisfy conditions ofthe outgassing rate and the water absorption rate. As a result,polyethylene resin (PE) is inappropriate to be used due to its highoutgassing rate and its low compressive strength.Polychlorotrifluoroethylene (PCTFE) is not used due to its remarkablyhigh price. Polyether ether ketone (PEEK) is inappropriate to be useddue to its high outgassing rate. Accordingly, it is determined that thata resin selected from the group consisting of polycarbonate (PC), glassfiber PC, low outgassing PC, polyphenylene sulfide (PPS), and liquidcrystal polymer (LCP) may be used as the material of the supportingunit. However, an outgassing rate of the PC is 0.19, which is at a lowlevel. Hence, as the time required to perform baking in which exhaustionis performed by applying heat is increased to a certain level, the PCmay be used as the material of the supporting unit.

The present inventor has found an optimal material by performing variousstudies on resins expected to be used inside the vacuum space part.Hereinafter, results of the performed studies will be described withreference to the accompanying drawings.

FIG. 5 is a view illustrating results obtained by performing anexperiment on vacuum maintenance performances of the resins. Referringto FIG. 5 , there is illustrated a graph showing results obtained byfabricating the supporting unit using the respective resins and thentesting vacuum maintenance performances of the resins. First, asupporting unit fabricated using a selected material was cleaned usingethanol, left at a low pressure for 48 hours, exposed to air for 2.5hours, and then subjected to an exhaust process at 90° C. for about 50hours in a state that the supporting unit was put in the vacuumadiabatic body, thereby measuring a vacuum maintenance performance ofthe supporting unit.

It may be seen that in the case of the LCP, its initial exhaustperformance is best, but its vacuum maintenance performance is bad. Itmay be expected that this is caused by sensitivity of the LCP totemperature. Also, it is expected through characteristics of the graphthat, when a final allowable pressure is 5×10-3 Torr, its vacuumperformance will be maintained for a time of about 0.5 year. Therefore,the LCP is inappropriate as the material of the supporting unit.

It may be seen that, in the case of the glass fiber PC (G/F PC), itsexhaust speed is fast, but its vacuum maintenance performance is low. Itis determined that this will be influenced by an additive. Also, it isexpected through the characteristics of the graph that the glass fiberPC will maintain its vacuum performance will be maintained under thesame condition for a time of about 8.2 years. Therefore, the LCP isinappropriate as the material of the supporting unit.

It is expected that, in the case of the low outgassing PC (L/O PC), itsvacuum maintenance performance is excellent, and its vacuum performancewill be maintained under the same condition for a time of about 34years, as compared with the above-described two materials. However, itmay be seen that the initial exhaust performance of the low outgassingPC is low, and therefore, fabrication efficiency of the low outgassingPC is lowered.

It may be seen that, in the case of the PPS, its vacuum maintenanceperformance is remarkably excellent, and its exhaust performance is alsoexcellent. Therefore, it is considered that, based on the vacuummaintenance performance, the PPS is used as the material of thesupporting unit.

FIGS. 6A-6C illustrate results obtained by analyzing components of gasesdischarged from the PPS and the low outgassing PC, in which thehorizontal axis represents mass numbers of gases and the vertical axisrepresents concentrations of gases. FIG. 6A illustrates a resultobtained by analyzing a gas discharged from the low outgassing PC. InFIG. 6A, it may be seen that H₂ series (I), H₂O series (II),N₂/CO/CO₂/O₂ series (III), and hydrocarbon series (IV) are equallydischarged. FIG. 6B illustrates a result obtained by analyzing a gasdischarged from the PPS. In FIG. 6B, it may be seen that H₂ series (I),H₂O series (II), and N₂/CO/CO₂/O₂ series (III) are discharged to a weakextent. FIG. 6C is a result obtained by analyzing a gas discharged fromstainless steel. In FIG. 6C, it may be seen that a similar gas to thePPS is discharged from the stainless steel. Consequently, it may be seenthat the PPS discharges a similar gas to the stainless steel. As theanalyzed result, it may be re-confirmed that the PPS is excellent as thematerial of the supporting unit.

FIG. 7 illustrates results obtained by measuring maximum deformationtemperatures at which resins are damaged by atmospheric pressure inhigh-temperature exhaustion. The bars 31 were provided at a diameter of2 mm at a distance of 30 mm. Referring to FIG. 7 , it may be seen that arupture occurs at 60° C. in the case of the PE, a rupture occurs at 90°C. in the case of the low outgassing PC, and a rupture occurs at 125° C.in the case of the PPS. As the analyzed result, it may be seen that thePPS is most used as the resin used inside of the vacuum space part.However, the low outgassing PC may be used in terms of fabrication cost.

A radiation resistance sheet 32 for reducing heat radiation between thefirst and second plate members 10 and 20 through the vacuum space part50 will be described. The first and second plate members 10 and 20 maybe made of a stainless material capable of preventing corrosion andproviding a sufficient strength. The stainless material has a relativelyhigh emissivity of 0.16, and hence a large amount of radiation heat maybe transferred. In addition, the supporting unit 30 made of the resinhas a lower emissivity than the plate members, and is not entirelyprovided to inner surfaces of the first and second plate members 10 and20. Hence, the supporting unit 30 does not have great influence onradiation heat. Therefore, the radiation resistance sheet 32 may beprovided in a plate shape over a majority of the area of the vacuumspace part 50 so as to concentrate on reduction of radiation heattransferred between the first and second plate members 10 and 20. Aproduct having a low emissivity may be used as the material of theradiation resistance sheet 32. In an embodiment, an aluminum foil havingan emissivity of 0.02 may be used as the radiation resistance sheet 32.Also, as the transfer of radiation heat may not be sufficiently blockedusing one radiation resistance sheet, at least two radiation resistancesheets 32 may be provided at a certain distance so as not to contacteach other. Also, at least one radiation resistance sheet may beprovided in a state in which it contacts the inner surface of the firstor second plate member 10 or 20.

Referring back to FIG. 3B, a distance between the plate members ismaintained by the supporting unit 30, and a porous material 33 may befilled in the vacuum space part 50. The porous material 33 may have ahigher emissivity than the stainless material of the first and secondplate members 10 and 20. However, as the porous material 33 is filled inthe vacuum space part 50, the porous material 33 has a high efficiencyfor resisting the radiation heat transfer.

FIGS. 8A-8C are views showing various embodiments of conductiveresistance sheets and peripheral parts thereof. Structures of theconductive resistance sheets are briefly illustrated in FIG. 2 , butwill be understood in detail with reference to the drawings.

First, a conductive resistance sheet proposed in FIG. 8A may be appliedto the main body-side vacuum adiabatic body. Specifically, the first andsecond plate members 10 and 20 are to be sealed so as to vacuumize theinterior of the vacuum adiabatic body. In this case, as the two platemembers have different temperatures from each other, heat transfer mayoccur between the two plate members. Conductive resistance sheet 60 isprovided to prevent heat conduction between two different kinds of platemembers.

The conductive resistance sheet 60 may be provided with sealing parts 61at which both ends of the conductive resistance sheet 60 are sealed todefining at least one portion of the wall for the third space andmaintain the vacuum state. The conductive resistance sheet 60 may beprovided as a thin foil in unit of micrometer so as to reduce the amountof heat conducted along the wall for the third space. The sealing parts610 may be provided as welding parts. That is, the conductive resistancesheet 60 and the plate members 10 and 20 may be fused to each other. Inorder to cause a fusing action between the conductive resistance sheet60 and the plate members 10 and 20, the conductive resistance sheet 60and the plate members 10 and 20 may be made of the same material, and astainless material may be used as the material. The sealing parts 610are not limited to the welding parts, and may be provided through aprocess, such as cocking. The conductive resistance sheet 60 may beprovided in a curved shape. Thus, a heat conduction distance of theconductive resistance sheet 60 is provided longer than a linear distanceof each plate member, so that the amount of heat conduction may befurther reduced.

A change in temperature occurs along the conductive resistance sheet 60.Therefore, in order to block heat transfer to the exterior of theconductive resistance sheet 60, a shielding part (shield) 62 may beprovided at an exterior of the conductive resistance sheet 60 such thatan adiabatic action occurs. In other words, in the refrigerator, thesecond plate member 20 has a high temperature and the first plate member10 has a low temperature. In addition, heat conduction from hightemperature to low temperature occurs in the conductive resistance sheet60, and hence, the temperature of the conductive resistance sheet 60 issuddenly changed. Therefore, when the conductive resistance sheet 60 isopened to the exterior thereof, heat transfer through the opened placemay seriously occur. In order to reduce heat loss, the shielding part 62is provided at the exterior of the conductive resistance sheet 60. Forexample, when the conductive resistance sheet 60 is exposed to any oneof the low-temperature space and the high-temperature space, theconductive resistance sheet 60 does not serve as a conductive resistoras well as the exposed portion thereof.

The shielding part 62 may be provided as a porous material contacting anouter surface of the conductive resistance sheet 60. The shielding part62 may be provided as an adiabatic structure, e.g., a separate gasket,which is placed at the exterior of the conductive resistance sheet 60.The shielding part 62 may be provided as a portion of the vacuumadiabatic body, which is provided at a position facing a correspondingconductive resistance sheet 60 when the main body-side vacuum adiabaticbody is closed with respect to the door-side vacuum adiabatic body. Inorder to reduce heat loss even when the main body and the door areopened, the shielding part 62 may be provided as a porous material or aseparate adiabatic structure.

A conductive resistance sheet proposed in FIG. 8B may be applied to thedoor-side vacuum adiabatic body. In FIG. 8B, portions different fromthose of FIG. 8A are described, and the same description is applied toportions identical to those of FIG. 8A. A side frame 70 is furtherprovided at an outside of the conductive resistance sheet 60. A part forsealing between the door and the main body, an exhaust port necessaryfor an exhaust process, a getter port for vacuum maintenance, forexample, may be placed on the side frame 70. This is because mounting ofparts is convenient in the main body-side vacuum adiabatic body, butmounting positions of parts are limited in the door-side vacuumadiabatic body.

In the door-side vacuum adiabatic body, it is difficult to place theconductive resistance sheet 60 at a front end portion (front end) of thevacuum space part, i.e., a corner side portion (corner side) of thevacuum space part. This is because, unlike the main body, a corner edgeportion (corner edge) of the door is exposed to the exterior. Morespecifically, if the conductive resistance sheet 60 is placed at thefront end portion of the vacuum space part, the corner edge portion ofthe door is exposed to the exterior, and hence, there is a disadvantagein that a separate adiabatic part should be configured so as toheat-insulate the conductive resistance sheet 60.

A conductive resistance sheet proposed in FIG. 8C may be installed inthe pipeline passing through the vacuum space part. In FIG. 8C, portionsdifferent from those of FIGS. 8A and 8B are described, and the samedescription is applied to portions identical to those of FIGS. 8A and8B. A conductive resistance sheet having the same shape as that of FIG.8A, a wrinkled conductive resistance sheet 63 may be provided at aperipheral portion of the pipeline 64. Accordingly, a heat transfer pathmay be lengthened, and deformation caused by a pressure difference maybe prevented. In addition, a separate shielding part may be provided toimprove adiabatic performance of the conductive resistance sheet.

A heat transfer path between the first and second plate members 10 and20 will be described with reference back to FIG. 8A. Heat passingthrough the vacuum adiabatic body may be divided into surface conductionheat conducted along a surface of the vacuum adiabatic body, morespecifically, the conductive resistance sheet 60, supporter conductionheat conducted along the supporting unit 30 provided inside of thevacuum adiabatic body, gas conduction heat conducted through an internalgas in the vacuum space part, and radiation transfer heat transferredthrough the vacuum space part.

The transfer heat may be changed depending on various depending onvarious design dimensions. For example, the supporting unit may bechanged such that the first and second plate members 10 and 20 mayendure a vacuum pressure without being deformed, the vacuum pressure maybe changed, a distance between the plate members may be changed, and alength of the conductive resistance sheet may be changed. The transferheat may be changed depending on a difference in temperature between thespaces (the first and second spaces) respectively provided by the platemembers. In the embodiment, a configuration of the vacuum adiabatic bodyhas been found by considering that its total heat transfer amount issmaller than that of a typical adiabatic structure formed by foamingpolyurethane. In a typical refrigerator including the adiabaticstructure formed by foaming the polyurethane, an effective heat transfercoefficient may be proposed as 19.6 mW/mK.

By performing a relative analysis on heat transfer amounts of the vacuumadiabatic body of the embodiment, a heat transfer amount by the gasconduction heat may become smallest. For example, the heat transferamount by the gas conduction heat may be controlled to be equal to orsmaller than 4% of the total heat transfer amount. A heat transferamount by solid conduction heat defined as a sum of the surfaceconduction heat and the supporter conduction heat is largest. Forexample, the heat transfer amount by the solid conduction heat may reach75% of the total heat transfer amount. A heat transfer amount by theradiation transfer heat is smaller than the heat transfer amount by thesolid conduction heat but larger than the heat transfer amount of thegas conduction heat. For example, the heat transfer amount by theradiation transfer heat may occupy about 20% of the total heat transferamount.

According to such a heat transfer distribution, effective heat transfercoefficients (eK: effective K) (W/mK) of the surface conduction heat,the supporter conduction heat, the gas conduction heat, and theradiation transfer heat may have an order of Math Equation 1.

eKsolid conduction heat>eKradiation transfer heat>eKgas conductionheat  [Equation 1]

Here, the effective heat transfer coefficient (eK) is a value that maybe measured using a shape and temperature differences of a targetproduct. The effective heat transfer coefficient (eK) is a value thatmay be obtained by measuring a total heat transfer amount and atemperature at least one portion at which heat is transferred. Forexample, a calorific value (W) is measured using a heating source thatmay be quantitatively measured in the refrigerator, a temperaturedistribution (K) of the door is measured using heats respectivelytransferred through a main body and an edge of the door of therefrigerator, and a path through which heat is transferred is calculatedas a conversion value (m), thereby evaluating an effective heat transfercoefficient.

The effective heat transfer coefficient (eK) of the entire vacuumadiabatic body is a value given by k=QL/AΔT. Here, Q denotes a calorificvalue (W) and may be obtained using a calorific value of a heater. Adenotes a sectional area (m2) of the vacuum adiabatic body, L denotes athickness (m) of the vacuum adiabatic body, and ΔT denotes a temperaturedifference.

For the surface conduction heat, a conductive calorific value may beobtained through a temperature difference (ΔT) between an entrance andan exit of the conductive resistance sheet 60 or 63, a sectional area(A) of the conductive resistance sheet, a length (L) of the conductiveresistance sheet, and a thermal conductivity (k) of the conductiveresistance sheet (the thermal conductivity of the conductive resistancesheet is a material property of a material and may be obtained inadvance). For the supporter conduction heat, a conductive calorificvalue may be obtained through a temperature difference (ΔT) between anentrance and an exit of the supporting unit 30, a sectional area (A) ofthe supporting unit, a length (L) of the supporting unit, and a thermalconductivity (k) of the supporting unit. Here, the thermal conductivityof the supporting unit is a material property of a material and may beobtained in advance. The sum of the gas conduction heat, and theradiation transfer heat may be obtained by subtracting the surfaceconduction heat and the supporter conduction heat from the heat transferamount of the entire vacuum adiabatic body. A ratio of the gasconduction heat, and the radiation transfer heat may be obtained byevaluating radiation transfer heat when no gas conduction heat exists byremarkably lowering a vacuum degree of the vacuum space part 50.

When a porous material is provided inside the vacuum space part 50,porous material conduction heat may be a sum of the supporter conductionheat and the radiation transfer heat. The porous material conductionheat may be changed depending on various variables including a kind, andan amount, for example, of the porous material.

According to an embodiment, a temperature difference ΔT1 between ageometric center formed by adjacent bars 31 and a point at which each ofthe bars 31 is located may be provided to be less than 0.5° C. Also, atemperature difference ΔT2 between the geometric center formed by theadjacent bars 31 and an edge portion of the vacuum adiabatic body may beprovided to be less than 0.5° C. In the second plate member 20, atemperature difference between an average temperature of the secondplate and a temperature at a point at which a heat transfer path passingthrough the conductive resistance sheet 60 or 63 meets the second platemay be largest. For example, when the second space is a region hotterthan the first space, the temperature at the point at which the heattransfer path passing through the conductive resistance sheet meets thesecond plate member becomes lowest. Similarly, when the second space isa region colder than the first space, the temperature at the point atwhich the heat transfer path passing through the conductive resistancesheet meets the second plate member becomes highest.

This means that the amount of heat transferred through other pointsexcept the surface conduction heat passing through the conductiveresistance sheet should be controlled, and the entire heat transferamount satisfying the vacuum adiabatic body may be achieved only whenthe surface conduction heat occupies the largest heat transfer amount.To this end, a temperature variation of the conductive resistance sheetmay be controlled to be larger than that of the plate member.

Physical characteristics of the parts constituting the vacuum adiabaticbody will be described. In the vacuum adiabatic body, a force by vacuumpressure is applied to all of the parts. Therefore, a material having astrength (N/m2) of a certain level may be used.

Under such circumferences, the plate members 10 and 20 and the sideframe 70 may be made of a material having a sufficient strength withwhich they are not damaged by even vacuum pressure. For example, whenthe number of bars 31 is decreased so as to limit support conductionheat, deformation of the plate member occurs due to the vacuum pressure,which may negatively influence the external appearance of refrigerator.The radiation resistance sheet 32 may be made of a material that has alow emissivity and may be easily subjected to thin film processing.Also, the radiation resistance sheet 32 is to ensure a sufficientstrength not to be deformed by an external impact. The supporting unit30 is provided with a strength sufficient so as to support the force ofthe vacuum pressure and endure an external impact, and is to havemachinability. The conductive resistance sheet 60 may be made of amaterial that has a thin plate shape and may endure the vacuum pressure.

In an embodiment, the plate member, the side frame, and the conductiveresistance sheet may be made of stainless materials having the samestrength. The radiation resistance sheet may be made of aluminum havinga weaker strength that the stainless materials. The supporting unit maybe made of resin having a weaker strength than the aluminum.

Unlike the strength from the point of view of materials, analysis fromthe point of view of stiffness is required. The stiffness (N/m) is aproperty that would not be easily deformed. Although the same materialis used, its stiffness may be changed depending on its shape. Theconductive resistance sheets 60 or 63 may be made of a material having astrength, but the stiffness of the material is low so as to increaseheat resistance and minimize radiation heat as the conductive resistancesheet is uniformly spread without any roughness when the vacuum pressureis applied. The radiation resistance sheet 32 requires a stiffness of acertain level so as not to contact another part due to deformation.Particularly, an edge portion (edge) of the radiation resistance sheetmay generate conduction heat due to drooping caused by self-load of theradiation resistance sheet. Therefore, a stiffness of a certain level isrequired. The supporting unit 30 requires a stiffness enough to endure acompressive stress from the plate member and an external impact.

In an embodiment, the plate member and the side frame may have thehighest stiffness so as to prevent deformation caused by the vacuumpressure. The supporting unit, particularly, the bar may have the secondhighest stiffness. The radiation resistance sheet may have a stiffnessthat is lower than that of the supporting unit but higher than that ofthe conductive resistance sheet. Lastly, the conductive resistance sheetmay be made of a material that is easily deformed by the vacuum pressureand has the lowest stiffness. Even when the porous material 33 is filledin the vacuum space part 50, the conductive resistance sheet may havethe lowest stiffness, and the plate member and the side frame may havethe highest stiffness.

The vacuum space part 50 may resist heat transfer by only the supportingunit 30. A porous material 33 may be filled within the supporting unit30 inside of the vacuum space part 50 to resist heat transfer. The heattransfer to the porous material 33 may resist without applying thesupporting unit 30.

In the above description, as a material suitable for the supportingunit, a resin of PPS has been proposed. The bar 31 is provided on thesupport plate 35 at intervals of 2 cm to 3 cm, and the bar 31 has aheight of 1 cm to 2 cm. These resins often have poor fluidity of theresin during molding. In many cases, the molded article does not havedesign value. Particularly, a shape of a molded product, such as a barhaving a short length, is often not provided properly due to non-uniforminjection of resin into a part far from a liquid injection port. Thismay cause damage to the supporting unit or a defective vacuum adiabaticbody later.

The supporting unit 30 is a substantially two-dimensional structure, butits area is considerably large. Therefore, if a defect occurs in one ofthe portions, it is difficult to discard the entire structure. Thislimitation becomes even more pronounced as refrigerators and warmingapparatus are becoming larger in size to meet the needs of consumers.

Hereinafter, a supporting unit for solving the above-describedlimitation will be described.

FIG. 9 is a view illustrating any one side portion of the supportingunit according an embodiment. Referring to FIG. 9 , one (first) sidesupport plate 350 is provided with at least two partial plates coupledto each other. In other words, partial plates having a small rectangularshape are coupled to each other to provide one side support plate 350having a large rectangular shape. For example, in the drawings, a secondpartial plate 352 and a fourth partial plate 354 are coupled to lowerand right sides of a first partial plate 351. The second partial plate352 and the fourth partial plate 354 are coupled to left and upper sidesof a third partial plate 353.

In an embodiment, the partial plates may have a same shape. Thus, a sizeof one side support plate 350 may reach four times the size of thepartial plate. When varying the number of partial plates 351, 352, 353and 354, which have the same shape and structure to be coupled to eachother, the size of the one side support plate 350 may be changed. It iseasily guessed that the size of the one side support plate 350 isdifferently provided depending on a size of the vacuum adiabatic body.

According to this configuration, the partial plate may be manufacturedusing resin having a poor fluidity when the partial plate is a liquidsuch as PPS, and the partial plate may be coupled. As the partial plateis small in size, defects may be prevented during molding, and even if amolding failure occurs, only the corresponding partial plate isdiscarded, so that it is not necessary to discard the whole supportplate.

After producing the small partial plate, it is assembled at an assemblysite of the vacuum adiabatic body and then put into the vacuum adiabaticbody. Thus, there is an advantage that handling and transportation areconvenient. In addition, it may be possible to prevent damage which mayoccur during handling of the large parts.

A plurality of small partial plates may be produced, and various typesof supporting units having a desired area may be obtained.

FIG. 10 is a plan view of the partial plate. Referring to FIG. 10 , thepartial plate 351 has one side base (base) 355 of a lattice structure,and a column 356 provided at a crossing point of the lattice on the oneside base 355. The one side base 355 may maintain the vacuum spaceinside of the plate members 10 and 20 by contacting inner surfaces ofthe plate members 10 and 20. The column 356 may provide a portion of thebar 31 to maintain an interval between the plate members 10 and 20.

A mesh end of the lattice structure constituting the one base 351 mayhave a male and female coupling structure for coupling different partialplates 351 to each other. For example, upper and left edges may have amale coupling structure, and right and lower edges may have a femalecoupling structure. Extension lines of arrows in the drawings indicateedges having the same coupling structure.

FIG. 11 is an enlarged view of a portion A of FIG. 10 . FIG. 12 is anenlarged view of a portion B of FIG. 10 .

Referring to FIGS. 11 and 12 , the male coupling structure (see FIG. 11) has an insertion part 357 at an end of a branch that provides thelattice of one base (base) 355. The insertion part 357 may be providedin a structure in which the end of the branch is extended. The malecoupling structure (see FIG. 12 ) may be provided with a holding part358 which is held at the end of the one base 355. A holding part 358 maybe provided with a recess 359 at the end of the branch. The shape of therecess 359 may be provided in a shape corresponding to the insertionpart 357. The insertion part 357 may be inserted into the recess 359.

The male coupling structure of the adjacent partial plate is verticallyaligned with the female coupling structure of the other partial plate,and the insertion part 357 and the recess 359 are used as a referencefor vertical alignment. Thereafter, when the insertion part 357 is movedin the vertical direction to the recess 359, coupling between thepartial plates may be completed. The vertical direction may be adirection perpendicular to the plane of a corresponding plate member.

For example, right and lower side male coupling structures of the firstpartial plate 351 are coupled to the male coupling structure of thefourth partial plate 354 and the male coupling structure of the secondpartial plate 352. This coupling structure may be the same for otherpartial plates.

The male coupling structure and the female coupling structure of thepartial plates allow for use of as small a quantity of resin as possibleand are intended to enable coupling while reducing size as much aspossible. Movement in one direction, i.e., up and down direction, ispermitted to be coupled. However, movement in the two-dimensionaldirection, i.e., in the area direction is not allowed, so that thecoupling is performed.

The male coupling structure and the female coupling structure do notneed to be completely fitted to each other, e.g., they are coupled toeach other. This is because not only the movement in the two-dimensionaldirection but also the vertical movement of the respective partialplates is permitted, but the vertical movements are fixed later by aseparate member. Also, this is because of characteristics of resinhaving poor liquid fluidity, it is necessary to make it easy to coupleslight loose coupling through movement in the up and down directionthrough the coupling. That is, this is because a numerical value of thecoupling structure for press-fitting may lead to damage to the partialplate at the time of coupling.

This structure reduces an amount of resin as much as possible to reducean amount of outgasing so as not to cause the limitation in vacuummaintenance of the vacuum space part and to prevent molding of the malecoupling structure and the female coupling structure from beingdifficult even if the resin having poor formability is used.

FIG. 13 is an enlarged view of a portion C of FIG. 9 . Referring to FIG.13 , in the case of the embodiment, all of the partial plates are incontact with each other, and the partial plates have the same shape. Theinsertion part 357 is fixed to the holding part 358 in a verticaldirection. The holding parts 358 and 357 provided on the respectivepartial plates 351, 352, 353 and 354 are coupled to each other so thatmovement of the partial plates in the two-dimensional direction, i.e.,one support plate 350 may provide a large area. The area of the one sidesupport plate 350 may be achieved by coupling a necessary number ofpartial plates. When varying the size and number of the partial plates,the sizes of the one side support plates 350 having various shapes andsizes may be obtained.

The column 356 provided at the intersection of the respective latticesconstituting the one base 355 may include two types. For example, thecolumns 356 may include a spacing (first) column 3561 that functions tomaintain an interval between the plate members 10 and 20 and a support(second) column 3562 that supports the radiation resistance sheet 32.

The spacing column 3561 is coupled to a groove (see reference numeral373 in FIG. 16 ) of the other support plate (see reference numeral 370in FIG. 14 ) to maintain the interval between the plate members 10 and20. In order to facilitate coupling with the groove 373 and to ensuremoldability using liquid resin, the spacing column 3561 is provided witha diameter H1 at a lower end of the spacing column, which is greaterthan a diameter H2 at an upper end. Although the cross-sectional shapeof the spacing column 3561 may not be circular, the cross-sectional sizeof the upper end may be small. However, the cross-sectional shape of thespacing column 3561 may be provided in a circular shape in order tosecure the forming shape of the spacing columns 3561 and the couplingbetween the spacing columns 3561 and the groove 373.

As in the case of the spacing column 3561, the support column 3562 has asmaller cross-sectional size of the support column 3562 toward the upperend for securing coupling and moldability. Further, for supporting theradiation resistance sheet 32, the support column 3562 may be providedwith a stepped protrusion 3563. A plurality of support columns 3562 maybe provided at predetermined intervals to stably support the radiationresistance sheet 32. The action of the support column 3562 will bedescribed in more detail below.

As has been described above, movement of the one side support plate 350in the vertical direction is restricted while the one side support plate350 is free to move in the vertical direction. Therefore, aconfiguration for limiting the vertical movement of each partial platemay be provided. The supporting unit 30 may be in contact with the innersurface of the plate member to support the interval of the plate members10 and 20. When the supporting unit is in contact with the plate member,point contact may provide a stable supporting force as compared withline contact. Therefore, a configuration may be provided such that thecolumn 356 does not directly contact the inner surface of the platemember.

In order to achieve this object, another side support plate 370corresponding to the one side support plate 350 may be further provided.Hereinafter, the one side support plate 350 and the other side supportplate 370 will be described.

FIG. 14 is a view for explaining coupling between one side support plateand the other side support plate. Referring to FIG. 14 , at least two ofthe partial plates are coupled to each other to provide the one sidesupport plate 350. The one side support plate 350 is restricted toseparate in the area (lateral) direction, but the upward and downward(vertical) movement is not restricted. In order to restrict verticalseparation of the one side support plate 350 and securely secure theinterval of the plate members 10 and 20 while more strongly coupling theone side support plate 350 in the direction of the area separation, asupport plate 370 is provided. The other side support plate 370 may becoupled to the one side support plate 350.

The other side support plate 370 may be understood as a member forsupporting the plate member opposite to the plate member supported bythe one side support plate 350. The other side support plate 370 may beused as it is with a standardized other side plate member having apredetermined size, or a standardized side plate member may be separatedat a proper position by cutting, for example. Therefore, it may beunderstood that the other plate member has the same configuration, butthe applied area is different.

Of course, the other side plate member as a unit having an areacorresponding to the one side support plate 350 may be provided, but asame constitution as the embodiment may be presented in order tomaximize the effect as a part.

In an embodiment, the other side plate member of the original size whichis not cut is formed at a center portion of the one side support plate350 at which the partial plates 351, 352, 353 and 354 are coupled toeach other as overlapping other side plates (boundary support plate)371. In this case, the other plate member is coupled to overlap aboundary of the different partial plates, thereby enhancing a bindingforce between the respective partial plates and performing the functionof restricting movement in the area direction. In this case, it isneedless to say that the function of restricting the movement of thepartial plate in the vertical direction and the function of maintainingthe interval of the plate members 10 and 20 are performed.

In other words, the boundary of each partial plate constituting onesupport plate and the other plate member constituting the other supportplate (which may include both of the overlapping other plate and thesingle other plate) cross each other and do not overlap each otherdesirable. If the boundaries overlap each other, there is a possibilitythat the members of the respective support plates, i.e., the partialplate and the other plate member are separated from each otherindependently or together.

The other plate member may be provided in the same shape as theoverlapping plate 371 coupled to the center portion of the one sidesupport plate 350. The other plate member may be coupled to the singlepartial plate without overlapping at least two of the partial plates. Inthis case, a portion of the other side plate member may be referred toas a single other side plate (secondary support plate) 372. In thiscase, it is needless to say that the function of restricting themovement of the partial plate in the vertical direction and the functionof maintaining the interval of the plate members 10 and 20 areperformed. However, it is not possible to perform the action ofrestricting movement of each partial plate in the direction of the areaand enhancing the binding force between the partial plates.

In the case of an embodiment, four other plate members 370 having thesame area as the partial plates 351, 352, 353, and 354 may be used. Oneof the four support plates 350 is coupled to a center of the othersupport plate 350 as the overlapping second side plate 371, and two ofthe four plates are cut horizontally and vertically and coupled as theoverlapping second side plate 371 to correspond to the center of thefour edges of the other side support plate 350. Among these, the platewhich is separated horizontally and vertically is omitted in order toprevent the drawing from being complicated. One of the four plates maybe quadrupled and coupled as a single other plate 372 corresponding tothe vertex portion of the other support plate 350.

As described above, the other side plate member may include alarger-sized other side plate member and a small-sized side plate memberderived from the standardized largest other side plate by separation andtransmission. According to this configuration, it is possible to providethe other side support plate of various shapes and structures withoutproviding a separate second side plate member according to the shape andshape of the vacuum adiabatic body.

The arrangement of the partial plate and the other plate member may bean embodiment, and those skilled in the art may suggest otherembodiments included in the scope of the same concept.

FIG. 15 is an enlarged view illustrating a portion D of FIG. 14 .Referring to FIG. 15 , the other side support plate 370 has alattice-shaped other side base 378 like the one side support plate 350and a groove 373 which is coupled to the column 356 at the intersectionof the lattice of the other side base 378.

A radiation resistance sheet 32 may be supported between the steppedprotrusion 3563 and the groove 373. Upper and lower positions of theradiation resistance sheet 32 may be restrained between the groove 373and the end of the stepped protrusion 3563 and the movement in thedirection of the area may be restricted by the support columns 3562.

FIG. 16 is a cross-sectional view taken along line XVI-XVI′ of FIG. 15 .Referring to FIG. 16 , a support position of the radiation resistancesheet 32 in the vertical direction is restricted between the steppedprotrusion 3563 and the groove 373. For this purpose, the size of thehole provided in the radiation resistance sheet 32 is smaller than thesize of the end of the stepped protrusion 3563 and the size of the endof the groove 373.

The vacuum adiabatic body may be manufactured in various sizes, andshapes. For example, the vacuum adiabatic body provided on the wall ofthe large refrigerator will be provided in a large plane, and the vacuumadiabatic body provided on the wall of the small refrigerator may beprovided in a small plane.

It is not advantageous to manufacture the respective support plates inorder to cope with refrigerator sizes of various shapes as describedabove because the cost of the products increases. This is because partstocks are increasing due to inability of parts to be shared, and it isdifficult to procure parts in the right place in response to demand. Inorder to cope with this limitation, the present inventor has proposed toutilize the partial plates 351, 352, 353, and 354, but it has beendifficult to cope with vacuum adiabatic bodies having various sizes bythe partial plate concept alone.

FIG. 17 is a view of a supporting unit according to another embodiment.Referring to FIG. 17 , the one side (first) support plate 3500 and theother side (second) support plate 3700 may be manufactured as two kindsof partial plates. The partial plate may include a first type partialplate 4001 having a lateral length ratio of 3:5 and a second typepartial plate 4002 having a lateral length ratio of 4:10. Length ratiosof the partial plates 4001 and 4002 may vary, but are merely examples.In addition, although support plates having a length ratio of 1:1 in theleft and right (lateral) directions are assumed in the drawings, theembodiment is not limited thereto, and it is possible to provide asupport plate having various shapes and sizes according to a combinationof two partial plates.

The one side support plate 3500 and the other side support plate 3700may be provided in a state of being rotated by 90 degrees from eachother. Due to such a configuration, it is possible to prevent loweringof a coupling force at a portion at which the partial plate isconnected.

The coupling between the one side support plate 3500 and the partialplate placed inside of the other side support plate 3700 may be appliedas it is in the embodiments already described.

In this embodiment, when a virtual line A-A is drawn in a directionalong edges of the one side support plate 3500 and the other sidesupport plate 3700, the following features are revealed. In the figures,imaginary lines are considered on the other support plate. Similarresults may be obtained for one side support plate.

First, at least two partial plates in the line through which theimaginary line passes are the same. In an embodiment, there are twofirst type partial plates 4001. This may have a technical meaning toincrease commonality of parts. That is, as at least two identicalpartial plates are used, mass production of the same partial plate maybe induced.

Second, all of the partial plates are not the same in the line throughwhich the imaginary line passes. In the embodiment, not only the firsttype partial plate 4001 but also the second partial plate 4002 wereused. This is a technical idea necessary for obtaining one side or theother side support plate having various shapes and areas.

Third, at least two kinds of partial plates are used in the line throughwhich the imaginary line passes. According to this, it is possible toprovide a more various one side or the other side support plate, so thatit is possible to cope with vacuum adiabatic body of various shapes andsizes. By using the two partial plates, it is expected that vacuumadiabatic bodies having various shapes and sizes at present may bemanufactured while achieving commonality of the partial plates.According to the present embodiment, it may be seen that the cost isreduced by more actively sharing components with respect to vacuum heatinsulating bodies of various shapes and sizes.

Hereinafter, vacuum pressure of the vacuum adiabatic body will bedescribed.

FIG. 18 illustrates graphs showing changes in adiabatic performance andchanges in gas conductivity with respect to vacuum pressures by applyinga simulation. Referring to FIG. 18 , it may be seen that, as the vacuumpressure is decreased, i.e., as the vacuum degree is increased, a heatload in the case of only the main body (Graph 1) or in the case wherethe main body and the door are joined together (Graph 2) is decreased ascompared with that in the case of the typical product formed by foamingpolyurethane, thereby improving adiabatic performance. However, it maybe seen that a degree of improvement of the adiabatic performance isgradually lowered. Also, it may be seen that, as the vacuum pressure isdecreased, gas conductivity (Graph 3) is decreased. However, it may beseen that, although the vacuum pressure is decreased, a ratio at whichthe adiabatic performance and the gas conductivity are improved isgradually lowered. Therefore, the vacuum pressure is decreased as low aspossible. However, it takes a long time to obtain excessive vacuumpressure, and much cost is consumed due to excessive use of a getter. Inthe embodiment, an optimal vacuum pressure is proposed from theabove-described point of view.

FIG. 19 is a graph illustrating results obtained by observing a time anda pressure in a process of exhausting the inside of the vacuum adiabaticbody when a supporting unit is used. Referring to FIG. 19 , in order tocreate the vacuum space part 50 to be in the vacuum state, a gas in thevacuum space part 50 is exhausted by a vacuum pump while evaporating alatent gas remaining in parts of the vacuum space part 50 throughbaking. However, if the vacuum pressure reaches a certain level or more,there exists a point at which the level of the vacuum pressure is notincreased any more (ΔT1). After that, the getter is activated bydisconnecting the vacuum space part 50 from the vacuum pump and applyingheat to the vacuum space part 50 (ΔT2). If the getter is activated, thepressure in the vacuum space part 50 is decreased for a certain periodof time, but then normalized to maintain a vacuum pressure of a certainlevel. The vacuum pressure that maintains the certain level afteractivation of the getter is approximately 1.8×10-6 Torr.

In the embodiment, a point at which the vacuum pressure is notsubstantially decreased any more even though the gas is exhausted byoperating the vacuum pump is set to a lowest limit of the vacuumpressure used in the vacuum adiabatic body, thereby setting a minimuminternal pressure of the vacuum space part 50 to 1.8×10-6 Torr.

FIG. 20 is a graph obtained by comparing a vacuum pressure with gasconductivity. Referring to FIG. 20 , gas conductivities with respect tovacuum pressures depending on sizes of a gap in the vacuum space part 50are represented as graphs of effective heat transfer coefficients (eK).Effective heat transfer coefficients (eK) were measured when the gap inthe vacuum space part 50 has three sizes of 2.76 mm, 6.5 mm, and 12.5mm. The gap in the vacuum space part 50 is defined as follows. When theradiation resistance sheet 32 exists inside of the vacuum space part 50,the gap is a distance between the radiation resistance sheet 32 and theplate member adjacent thereto. When the radiation resistance sheet 32does not exist inside of the vacuum space part 50, the gap is a distancebetween the first and second plate members.

It was seen that, as the size of the gap is small at a pointcorresponding to a typical effective heat transfer coefficient of 0.0196W/mK, which is provided to an adiabatic material formed by foamingpolyurethane, the vacuum pressure is 2.65×10-1 Torr even when the sizeof the gap is 2.76 mm. It was seen that the point at which reduction inadiabatic effect caused by gas conduction heat is saturated even thoughthe vacuum pressure is decreased is a point at which the vacuum pressureis approximately 4.5×10-3 Torr. The vacuum pressure of 4.5×10-3 Torr maybe defined as the point at which the reduction in adiabatic effectcaused by gas conduction heat is saturated. Also, when the effectiveheat transfer coefficient is 0.1 W/mK, the vacuum pressure is 1.2×10-2Torr.

When the vacuum space part 50 is not provided with the supporting unitbut provided with the porous material, the size of the gap ranges from afew micrometers to a few hundreds of micrometers. In this case, theamount of radiation heat transfer is small due to the porous materialeven when the vacuum pressure is relatively high, i.e., when the vacuumdegree is low. Therefore, an appropriate vacuum pump is used to adjustthe vacuum pressure. The vacuum pressure appropriate to thecorresponding vacuum pump is approximately 2.0×10-4 Torr. Also, thevacuum pressure at the point at which the reduction in adiabatic effectcaused by gas conduction heat is saturated is approximately 4.7×10-2Torr. Also, the pressure where the reduction in adiabatic effect causedby gas conduction heat reaches the typical effective heat transfercoefficient of 0.0196 W/mK is 730 Torr.

When the supporting unit and the porous material are provided togetherin the vacuum space part, a vacuum pressure may be created and used,which is in the middle between the vacuum pressure when only thesupporting unit is used and the vacuum pressure when only the porousmaterial is used.

In the description of embodiments, a part for performing the same actionin each embodiment of the vacuum adiabatic body may be applied toanother embodiment by properly changing the shape or dimension offoregoing another embodiment. Accordingly, still another embodiment maybe easily proposed. For example, in the detailed description, in thecase of a vacuum adiabatic body suitable as a door-side vacuum adiabaticbody, the vacuum adiabatic body may be applied as a main body-sidevacuum adiabatic body by properly changing the shape and configurationof a vacuum adiabatic body.

The vacuum adiabatic body proposed in embodiments may be applied torefrigerators. However, the application of the vacuum adiabatic body isnot limited to the refrigerators, and may be applied in variousapparatuses, such as cryogenic refrigerating apparatuses, heatingapparatuses, and ventilation apparatuses.

According to embodiments, the vacuum adiabatic body may be industriallyapplied to various adiabatic apparatuses. The adiabatic effect may beenhanced, so that it is possible to improve energy use efficiency and toincrease the effective volume of an apparatus.

Any reference in this specification to “one embodiment,” “anembodiment,” “example embodiment,” etc., means that a particularfeature, structure, or characteristic described in connection with theembodiment is included in at least one embodiment of the invention. Theappearances of such phrases in various places in the specification arenot necessarily all referring to the same embodiment. Further, when aparticular feature, structure, or characteristic is described inconnection with any embodiment, it is submitted that it is within thepurview of one skilled in the art to effect such feature, structure, orcharacteristic in connection with other ones of the embodiments.

Although embodiments have been described with reference to a number ofillustrative embodiments thereof, it should be understood that numerousother modifications and embodiments can be devised by those skilled inthe art that will fall within the spirit and scope of the principles ofthis disclosure. More particularly, various variations and modificationsare possible in the component parts and/or arrangements of the subjectcombination arrangement within the scope of the disclosure, the drawingsand the appended claims. In addition to variations and modifications inthe component parts and/or arrangements, alternative uses will also beapparent to those skilled in the art.

What is claimed is:
 1. A vacuum adiabatic body, comprising: a firstplate: a second plate: a vacuum space provided between the first plateand the second plate; and a support configured to maintain a distancebetween the first plate and second plate, wherein the support isdisposed next to or adjacent to the first plate, and wherein the supportcomprises at least two partial plates coupled to each other.
 2. Thevacuum adiabatic body of the claim 1, wherein the support furthercomprises a support plate including the at least two partial plates andprovided in a plate structure or a lattice structure.
 3. The vacuumadiabatic body of claim 2, wherein the support plate is provided in thelattice structure, wherein a first partial plate of the at least twopartial plates includes a first base of the lattice structure and acolumn provided at an intersection of the lattice structure on the firstbase, wherein a second partial plate of the at least two partial platesincludes a second base of the lattice structure and a groove provided atthe intersection of the lattice structure on the second base, andwherein the groove is configured to receive the column.
 4. The vacuumadiabatic body of claim 2, wherein the support plate is provided in thelattice structure, and wherein an end of the lattice structure comprisesmale and female coupling structures that couple the at least two partialplates to each other.
 5. The vacuum adiabatic body of claim 4, wherein afirst partial plate of the at least two partial plates comprises a malecoupling structure having an insertion portion at the end, wherein asecond partial plate of the at least one partial plates comprises afemale coupling structure having a holding portion at the end, andwherein the holding portion is configured to catch the insertionportion.
 6. The vacuum adiabatic body according to claim 1, wherein afirst partial plate of the at least two partial plates comprises upperand left edges having a male coupling structure, and right and loweredges having a female coupling structure, and wherein the at least twopartial plates each have a small rectangular shape and are coupled toeach other to provide a side support plate having a large rectangularshape.
 7. The vacuum adiabatic body according to claim 1, wherein the atleast two partial plates extend along an extension direction of thefirst plate or the second plate.
 8. The vacuum adiabatic body accordingto claim 1, wherein the at least two partial plates have a same shape.9. The vacuum adiabatic body according to claim 1, wherein edges of afirst partial plate of the at least two partial plates have a malestructure, and wherein edges of a second partial plate of the at leasttwo partial plates have a female structure that matches the malestructure.
 10. The vacuum adiabatic body according to claim 1, whereinthe at least two partial plates each comprises a resin selected from thegroup consisting of polycarbonate (PC), glass fiber PC, low outgassingPC, polyphenylene sulfide (PPS), and liquid crystal polymer (LCP).
 11. Avacuum adiabatic body, comprising: a first plate: a second plate: avacuum space provided between the first plate and the second plate; anda support configured to maintain a distance between the first plate andsecond plate, wherein the support is disposed next to or adjacent to thefirst plate, and wherein the support comprises a bar that extends in adirection of a thickness of the vacuum space.
 12. The vacuum adiabaticbody according to claim 11, wherein the support further comprises asupport plate that extends in a direction of a width of the vacuumspace, and wherein the bar includes a spacing column provided at thesupport plate.
 13. The vacuum adiabatic body according to claim 12,wherein the support plate comprises at least two partial plates coupledto each other, wherein the spacing column is provided at a first partialplate of the at least two partial plates and is coupled to a secondpartial plate of the at least two partial plates.
 14. The vacuumadiabatic body according to claim 11, further comprising a radiationresistance sheet to reduce heat radiation between the first plate andsecond plate, wherein the radiation resistance sheet is disposed next toor adjacent to the first plate, and wherein the bar includes a supportcolumn configured to support the radiation resistance sheet.
 15. Thevacuum adiabatic body according to claim 11, wherein the bar includes afirst end having a first cross-sectional size and a second end having asecond cross-sectional size which is less than the first cross-sectionalsize, and wherein the first end is positioned adjacent to the firstplate and the second end is positioned adjacent to the second plate. 16.A vacuum adiabatic body, comprising: a first plate: a second plate: avacuum space provided between the first plate and the second plate; anda support configured to maintain a distance between the first plate andsecond plate, wherein the support is disposed next to or adjacent to thefirst plate, and wherein the support comprises a first support plateincluding at least two partial plates coupled to each other, and asecond support plate coupled to the first support plate.
 17. The vacuumadiabatic body according to claim 16, wherein the second support platecomprises at least one of: an overlapping support plate disposed tooverlap a boundary of the at least two partial plates; or a singlesupport plate disposed not to overlap the at least two partial plates.18. The vacuum adiabatic body according to claim 16, wherein the secondsupport plate comprises a first plate portion coupled to a center of thefirst support plate and at least one second plate portion provided atedges of the first plate portion.
 19. The vacuum adiabatic bodyaccording to claim 16, wherein when a virtual line is drawn from a firstedge of one of the first support plate or the second support plate in adirection toward a second edge thereof, the virtual line passes throughthe at least two partial plates, and wherein the at least two partialplates have a same shape.
 20. The vacuum adiabatic body according toclaim 16, wherein the first support plate is configured to contact oneof the first plate or the second plate, and wherein the second supportplate is configured to contact the other one of the first plate or thesecond plate.